US20140375014A1 - Trailing arm suspension beam assembly - Google Patents
Trailing arm suspension beam assembly Download PDFInfo
- Publication number
- US20140375014A1 US20140375014A1 US14/294,853 US201414294853A US2014375014A1 US 20140375014 A1 US20140375014 A1 US 20140375014A1 US 201414294853 A US201414294853 A US 201414294853A US 2014375014 A1 US2014375014 A1 US 2014375014A1
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- Prior art keywords
- recess
- weld
- trailing arm
- trailing
- located proximate
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- 239000000725 suspension Substances 0.000 title claims abstract description 29
- 210000005069 ears Anatomy 0.000 description 9
- 230000000712 assembly Effects 0.000 description 5
- 238000000429 assembly Methods 0.000 description 5
- 238000005266 casting Methods 0.000 description 4
- 230000008878 coupling Effects 0.000 description 3
- 238000010168 coupling process Methods 0.000 description 3
- 238000005859 coupling reaction Methods 0.000 description 3
- 238000003466 welding Methods 0.000 description 3
- 238000013459 approach Methods 0.000 description 1
- 230000037237 body shape Effects 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
Images
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G9/00—Resilient suspensions of a rigid axle or axle housing for two or more wheels
- B60G9/006—Resilient suspensions of a rigid axle or axle housing for two or more wheels the axle being connected to two trailing arms with only one of them being rigidly connected to the axle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G11/00—Resilient suspensions characterised by arrangement, location or kind of springs
- B60G11/26—Resilient suspensions characterised by arrangement, location or kind of springs having fluid springs only, e.g. hydropneumatic springs
- B60G11/28—Resilient suspensions characterised by arrangement, location or kind of springs having fluid springs only, e.g. hydropneumatic springs characterised by means specially adapted for attaching the spring to axle or sprung part of the vehicle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G7/00—Pivoted suspension arms; Accessories thereof
- B60G7/008—Attaching arms to unsprung part of vehicle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G7/00—Pivoted suspension arms; Accessories thereof
- B60G7/02—Attaching arms to sprung part of vehicle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G9/00—Resilient suspensions of a rigid axle or axle housing for two or more wheels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G9/00—Resilient suspensions of a rigid axle or axle housing for two or more wheels
- B60G9/003—Resilient suspensions of a rigid axle or axle housing for two or more wheels the axle being rigidly connected to a trailing guiding device
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2200/00—Indexing codes relating to suspension types
- B60G2200/30—Rigid axle suspensions
- B60G2200/31—Rigid axle suspensions with two trailing arms rigidly connected to the axle
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2202/00—Indexing codes relating to the type of spring, damper or actuator
- B60G2202/10—Type of spring
- B60G2202/15—Fluid spring
- B60G2202/152—Pneumatic spring
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2204/00—Indexing codes related to suspensions per se or to auxiliary parts
- B60G2204/10—Mounting of suspension elements
- B60G2204/12—Mounting of springs or dampers
- B60G2204/126—Mounting of pneumatic springs
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2204/00—Indexing codes related to suspensions per se or to auxiliary parts
- B60G2204/40—Auxiliary suspension parts; Adjustment of suspensions
- B60G2204/43—Fittings, brackets or knuckles
- B60G2204/4306—Bracket or knuckle for rigid axles, e.g. for clamping
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2206/00—Indexing codes related to the manufacturing of suspensions: constructional features, the materials used, procedures or tools
- B60G2206/01—Constructional features of suspension elements, e.g. arms, dampers, springs
- B60G2206/80—Manufacturing procedures
- B60G2206/82—Joining
- B60G2206/8201—Joining by welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60G—VEHICLE SUSPENSION ARRANGEMENTS
- B60G2206/00—Indexing codes related to the manufacturing of suspensions: constructional features, the materials used, procedures or tools
- B60G2206/01—Constructional features of suspension elements, e.g. arms, dampers, springs
- B60G2206/80—Manufacturing procedures
- B60G2206/82—Joining
- B60G2206/8207—Joining by screwing
Definitions
- the present invention relates to an axle suspension system for heavy vehicles, and in particular to a trailing arm assembly with increased strength and which is adapted to increase the durability of an associated vehicle axle.
- a variety of vehicle suspension systems utilizing air springs have been developed for use within semi-tractor trailer and other heavy duty vehicles. These systems control the relative position of the chassis with respect to an associated axle or axles and also to cushion the relative movement of the axle(s) toward the chassis frame.
- FIG. 1 is a perspective view of a suspension system that includes a trailing arm assembly embodying the present invention
- FIG. 2 is a side elevational view of the suspension system, wherein a braking assembly has been removed to better illustrate the trailing arm assembly;
- FIG. 3 is a perspective view of a first embodiment of the trailing arm assembly
- FIG. 4 is a side elevational view of the first embodiment of the trailing arm assembly
- FIG. 5 is a top plan view of the first embodiment of the trailing arm assembly
- FIG. 6 is a perspective view of an end of the first embodiment of the trailing arm assembly
- FIG. 7A is an enlarged, partial perspective view of the suspension system, and in particular the trailing arm assembly
- FIG. 7B is an enlarged, partial perspective view of the suspension system, and in particular the trailing arm assembly
- FIG. 8 is an enlarged side elevational view of the first embodiment of the trailing arm assembly
- FIG. 9 is a perspective view of a second embodiment of the trailing arm beam assembly.
- FIG. 10 is a perspective view of a trailing arm beam of the second embodiment of the trailing arm beam assembly
- FIG. 11 a is a rear perspective view of a spring support member of the second embodiment of the trailing arm beam assembly
- FIG. 11 b is a front perspective view of the spring support member of the second embodiment of the trailing arm beam assembly
- FIG. 12 is a perspective view of a third embodiment of the trailing arm assembly
- FIG. 13 is a side elevational view of the third embodiment of the trailing arm assembly
- FIG. 14 is a top plan view of the third embodiment of the trailing arm assembly
- FIG. 15 is a perspective view of a fourth embodiment of the trailing arm
- FIG. 16 is a side elevational view of the fourth embodiment of the trailing arm
- FIG. 17 is a partial cross-sectional top view of the fourth embodiment of the trailing arm taken along the line XVII-XVII, FIG. 16 ;
- FIG. 18 is a top plan view of a plurality of a fourth embodiment of the trailing arm positioned within a rectangular casting core box.
- the terms “upper,” “lower,” “right,” “left,” “rear,” “front,” “vertical,” “horizontal,” and derivatives thereof shall relate to the invention as oriented in FIGS. 1 and 2 .
- the invention may assume various alternative orientations and step sequences, except where expressly specified to the contrary.
- the specific devices and processes illustrated in the attached drawings, and described in the following specification are exemplary embodiments of the inventive concepts defined in the appended claims. Hence, specific dimensions and other physical characteristics relating to the embodiments disclosed herein are not to be considered as limiting, unless the claims expressly state otherwise.
- the reference numeral 10 ( FIGS. 1 and 2 ) generally designates a heavy duty vehicle suspension system that includes a plurality of trailing arm assemblies 12 each embodying the present invention.
- the vehicle suspension system 10 includes a pair of tandem axle assemblies including a forward axle assembly 14 and a rearward axle assembly 16 , respectively.
- Each of the axle assemblies 14 , 16 is supported by an associated trailing arm assembly 12 .
- Each trailing arm assembly 12 includes a trailing arm or beam 18 having a first end 20 and a second end 21 .
- the first end 20 is pivotally supported by an associated hanger bracket 22 that is fixedly attached to and extends downwardly from a longitudinally extending vehicle frame member 24 .
- first end 20 of the hanger bracket 22 is pivotally coupled to the associated hanger bracket 22 via a bushing assembly 25 to pivot about a pivot axis 26 .
- An air spring assembly 28 is positioned between an air spring support 30 of the trailing arm assembly 12 and the vehicle frame member 24 .
- each trailing arm assembly 12 includes the trailing arm 18 and the air spring support 30 .
- the trailing arm 18 includes a body portion 32 having a bushing aperture 34 located at the first end 20 , and an axle adapter 36 located at the second end 21 .
- the body portion 32 comprises a metal alloy, is preferably integrally cast as a single piece, and includes an I-shaped cross-sectional configuration including a vertical web portion 40 , a bottom flange 42 , and an upper flange 44 .
- the axle adapter 36 of the trailing arm 18 includes an outwardly, and specifically downwardly-opening, arcuately-shaped recess 46 that receives a vehicle axle 48 ( FIGS. 7A , 7 B) of the axle assembly 14 , 16 therein.
- the axle adapter 36 further includes a pair of laterally extending forward weld ears 50 and a pair of laterally extending rearward weld ears 52 .
- the recess 46 and the weld ears 50 , 52 cooperate to define an axle seat periphery 54 , about which the trailing arm 18 is welded to the associated axle 14 , 16 .
- a single continuous weld 55 is preferably applied about the entire length of the axle seat periphery, thereby reducing the number of weld ends and increasing the durability of the axle connection. Specifically, welding about the entire axle seat periphery between the axle adapter 36 and the axle 48 , reduces stress risers associated with using multiple welds, and allows a relatively thin axle wall to be utilized. As best illustrated in FIG.
- the forward weld ears 50 and rearward weld ears 52 are positioned and configured with regards to the associated axle 14 such that the weld 55 positioned proximate a leading edge 65 of the forward weld ears 50 preferably forms a negative angle a with the horizontal of between about 30° to about 45°, and more preferably of about 35°, and such that the weld 55 positioned proximate a trailing edge 67 of the rearward weld ears 52 preferably forms a positive angle ⁇ the horizontal of between about 25° and about 45°, and more preferably of about 8°, thereby reducing the stress exerted on the axle connection by typical operational loads.
- the location of the weld ears 50 , 52 , and thus the associated welds significantly reduces the stress swing exerted on the weld ears 50 , 52 and the welds 55 .
- the air spring support 30 ( FIGS. 3-6 ) of the trailing arm assembly 12 includes a top plate or spring support plate 56 upon which the associated air spring assembly 28 is supported, and a pair of support brackets 58 extending between the second end 21 of the trailing arm 18 and the top plate 56 .
- each support bracket 58 is generally triangularly shaped and includes a forward edge 60 weldably secured to a rearward face 61 of the second end 21 of the trailing beam 18 , a top edge 62 weldably secured to an underside of the top plate 56 , and a downwardly facing edge 64 .
- the top plate 56 is positioned with respect to the support brackets 58 such that a forward edge portion 66 of the top plate 56 overlies the upper flange 44 of the trailing arm 18 .
- the forward edge portion 66 includes a welding window 68 which receives a weld, thereby securing the top plate 56 to the trailing arm assembly 12 .
- the weld window 68 is located on an outboard side of the top plate 56 such that the top plate 56 is welded to a draft surface of the trailing arm 18 , thereby causing the top plate 56 to “tilt” to the outboard side of the trailing arm 18 .
- the spring supporting surface 57 of the top plate 56 is outwardly canted with regards to at least one of the central axis member 39 and the central axis of the pivot axis 26 at an angle ⁇ of preferably within the range of between about 0.5° and about 3°; and more preferably within the range of between about 0.5° and 1.5°.
- loading of the overall suspension system 10 causes the overall trailing arm assembly 12 to “tilt” inboard such that the top plate or air spring mounting plate 56 is substantially parallel to upper air spring mounting plates 70 ( FIG. 1 ) attached to the frame member 24 .
- the resulting parallel relationship between the top plate 56 and the associated upper air spring mounting plate 70 reduces the wear exerted on the air spring assembly 28 during operation.
- the reference numeral 12 a ( FIGS. 9-11 b ) generally designates another embodiment of the trailing arm assembly of the present invention. Since the trailing arm assembly 12 a is similar to the previously described embodiment of the trailing arm assembly 12 , similar parts appearing in FIGS. 1-8 and FIGS. 9-11 b respectively are represented by the same, corresponding reference numeral, except for the suffix “a” in the numerals of the latter.
- the trailing arm assembly 12 a includes the trailing arm 18 a and the air spring support 30 a .
- the second end 21 a of the trailing arm includes a pair of rearwardly extending eyelets or hinge members 100 having bolt-receiving apertures 102 extending therethrough.
- the air spring support 20 a is generally arcuately-shaped and includes a forwardly-extending coupling portion 104 and a rearwardly-located spring support plate 56 a .
- the coupling portion 104 includes a pair of laterally-spaced plate portions 106 that flank the hinge members 100 and include apertures 108 that correspond to the apertures 102 and that receive bolts 110 , thereby coupling the air spring support 20 a with the trailing arm member 18 a .
- the end surface 111 of the trailing arm 18 a is machined and abuts a machined surface 113 of the air spring support 30 a , so as to support downward forces exerted by the air spring 28 onto the air spring support 30 a.
- the reference numeral 12 b ( FIGS. 12-14 ) generally designates another embodiment of the trailing arm assembly of the present invention. Since the trailing arm assembly 12 b is similar to the previously described embodiment of the trailing arm assembly 12 , similar parts appearing in FIGS. 1-8 and FIGS. 12-14 respectively are represented by the same, corresponding reference numeral, except for the suffix “b” in the numerals of the latter.
- the trailing arm assembly 12 b includes the trailing arm 18 b and the air spring support 30 b .
- the second end 21 b of the trailing arm 18 b is rearwardly, downwardly sloped and is defined by a rearward surface 80 and a ledge 82 that is vertically offset below an uppermost surface of the trailing arm 18 b .
- each of the support brackets 58 b of the air spring support 30 b has a forwardly-opening concave shape that is positioned about a complimentary convex shape of the rearward surface 80 of the trailing arm 18 b .
- the forward edge portion 66 b of the top plate 56 b cantilevers and extends over the ledge 82 of the second end 21 b of the trailing arm 18 b and is secured thereto via a weld located within the welding window 68 b .
- the air spring support 30 b is further secured to the associated trailing arm 18 b via welds 84 , while the top plate 56 b and the support brackets 58 b are secured to one another via a plurality of welds 86 .
- This particular configuration allows the overall height of the trailing arm assembly 12 b to be minimized, and allows vertical loads from the air spring assemblies 28 to be supported by the trailing arm 18 b through compressive stresses within the ledge 82 and rearward surface 80 of the trailing arm 18 b.
- the reference numeral 18 c ( FIGS. 15-17 ) generally designates another embodiment of the trailing arm of the present invention. Since the trailing arm 18 c is similar to the previously described embodiment of the trailing arm 18 , similar parts appearing in FIGS. 3-6 and FIGS. 15-17 respectively are represented by the same, corresponding reference numeral, except for the suffix “c” in the numerals of the latter. As best illustrated in FIGS. 16 and 17 , the overall height h defined between an uppermost portion of the recess 46 c and the substantially perpendicularly located upper surface of the trailing arm 18 c is reduced.
- This reduction in overall height is accomplished by providing a relatively thick portion 40 c ′ to the web portion 40 c of the trailing arm 18 c proximate the recess 46 c , whereat the portion 40 c of the web portion 40 c has a relatively greater thickness t′′ compared to the thickness t′ of the web portion 40 c extending along the remaining length of the trailing beam 18 c .
- the thickness t′′ is between 2 and 8 times greater than the thickness t′.
- the trailing arm 18 c does not include vertically extending reinforcement webs proximate to the forward edge of the recess 46 c , thereby providing a reduction in the overall weight of the trailing arm 18 c.
- the reference numeral 18 d ( FIG. 18 ) generally designates yet another embodiment of the trailing arm of the present invention. Since the trailing arm 18 d is similar to the previously described embodiment of the trailing arm 18 , similar parts appearing in FIGS. 3-6 and FIG. 18 respectively are represented by the same, corresponding reference numeral, except for the suffix “d” in the numerals of the latter.
- the trailing arm 18 d is provided with an overall curvalinear body shape thereby allowing “nesting” of a plurality of trailing arms 18 d with one another within an associated casting core box 88 . The nesting of the trailing arms 18 d with one another reduces the overall area required within the casting core box 88 , thereby increasing yield per mold during the casting process, resulting in a reduction in costs for manufacturing each beam and increasing the overall efficiency of the foundry.
- the present inventive trailing arm assembly and related suspension system increases the durability of the associated axle connection, while simultaneously reducing the weight.
- the trailing arm assembly and suspension system is efficient in assembly and use, is capable of a long operating life, and is particularly well adapted for the proposed use.
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Abstract
Description
- The present invention relates to an axle suspension system for heavy vehicles, and in particular to a trailing arm assembly with increased strength and which is adapted to increase the durability of an associated vehicle axle.
- A variety of vehicle suspension systems utilizing air springs have been developed for use within semi-tractor trailer and other heavy duty vehicles. These systems control the relative position of the chassis with respect to an associated axle or axles and also to cushion the relative movement of the axle(s) toward the chassis frame. The suspension systems, and particularly the components such as the trailing arms and axle assemblies thereof, undergo significant stress during operation of the vehicle. Specifically, the connection between the trailing arms and the associated axle undergo significant stress when typical operational loads are exerted thereon, both in the vertical and lateral directions. While many systems have been developed to reduce such stress, previous approaches have been relatively expensive, and at times only marginally effective.
- There is a need for a lightweight and inexpensive air spring suspension system that reduces the stress exerted between the trailing arms of the suspension system and the associated axle.
- In the drawings:
-
FIG. 1 is a perspective view of a suspension system that includes a trailing arm assembly embodying the present invention; -
FIG. 2 is a side elevational view of the suspension system, wherein a braking assembly has been removed to better illustrate the trailing arm assembly; -
FIG. 3 is a perspective view of a first embodiment of the trailing arm assembly; -
FIG. 4 is a side elevational view of the first embodiment of the trailing arm assembly; -
FIG. 5 is a top plan view of the first embodiment of the trailing arm assembly; -
FIG. 6 is a perspective view of an end of the first embodiment of the trailing arm assembly; -
FIG. 7A is an enlarged, partial perspective view of the suspension system, and in particular the trailing arm assembly; -
FIG. 7B is an enlarged, partial perspective view of the suspension system, and in particular the trailing arm assembly; -
FIG. 8 is an enlarged side elevational view of the first embodiment of the trailing arm assembly; -
FIG. 9 is a perspective view of a second embodiment of the trailing arm beam assembly; -
FIG. 10 is a perspective view of a trailing arm beam of the second embodiment of the trailing arm beam assembly; -
FIG. 11 a is a rear perspective view of a spring support member of the second embodiment of the trailing arm beam assembly; -
FIG. 11 b is a front perspective view of the spring support member of the second embodiment of the trailing arm beam assembly; -
FIG. 12 is a perspective view of a third embodiment of the trailing arm assembly; -
FIG. 13 is a side elevational view of the third embodiment of the trailing arm assembly; -
FIG. 14 is a top plan view of the third embodiment of the trailing arm assembly; -
FIG. 15 is a perspective view of a fourth embodiment of the trailing arm; -
FIG. 16 is a side elevational view of the fourth embodiment of the trailing arm; -
FIG. 17 is a partial cross-sectional top view of the fourth embodiment of the trailing arm taken along the line XVII-XVII,FIG. 16 ; and, -
FIG. 18 is a top plan view of a plurality of a fourth embodiment of the trailing arm positioned within a rectangular casting core box. - For purposes of description herein, the terms “upper,” “lower,” “right,” “left,” “rear,” “front,” “vertical,” “horizontal,” and derivatives thereof shall relate to the invention as oriented in
FIGS. 1 and 2 . However, it is to be understood that the invention may assume various alternative orientations and step sequences, except where expressly specified to the contrary. It is also to be understood that the specific devices and processes illustrated in the attached drawings, and described in the following specification are exemplary embodiments of the inventive concepts defined in the appended claims. Hence, specific dimensions and other physical characteristics relating to the embodiments disclosed herein are not to be considered as limiting, unless the claims expressly state otherwise. - The reference numeral 10 (
FIGS. 1 and 2 ) generally designates a heavy duty vehicle suspension system that includes a plurality oftrailing arm assemblies 12 each embodying the present invention. In the illustrated example, thevehicle suspension system 10 includes a pair of tandem axle assemblies including aforward axle assembly 14 and arearward axle assembly 16, respectively. Each of theaxle assemblies trailing arm assembly 12. Eachtrailing arm assembly 12 includes a trailing arm orbeam 18 having afirst end 20 and asecond end 21. Thefirst end 20 is pivotally supported by an associatedhanger bracket 22 that is fixedly attached to and extends downwardly from a longitudinally extendingvehicle frame member 24. Specifically, thefirst end 20 of thehanger bracket 22 is pivotally coupled to the associatedhanger bracket 22 via abushing assembly 25 to pivot about apivot axis 26. Anair spring assembly 28 is positioned between anair spring support 30 of thetrailing arm assembly 12 and thevehicle frame member 24. - As best illustrated in
FIGS. 3-6 , eachtrailing arm assembly 12 includes thetrailing arm 18 and theair spring support 30. Thetrailing arm 18 includes abody portion 32 having abushing aperture 34 located at thefirst end 20, and anaxle adapter 36 located at thesecond end 21. Thebody portion 32 comprises a metal alloy, is preferably integrally cast as a single piece, and includes an I-shaped cross-sectional configuration including avertical web portion 40, abottom flange 42, and anupper flange 44. - The
axle adapter 36 of thetrailing arm 18 includes an outwardly, and specifically downwardly-opening, arcuately-shaped recess 46 that receives a vehicle axle 48 (FIGS. 7A , 7B) of theaxle assembly axle adapter 36 further includes a pair of laterally extendingforward weld ears 50 and a pair of laterally extending rearwardweld ears 52. Therecess 46 and theweld ears axle seat periphery 54, about which thetrailing arm 18 is welded to the associatedaxle continuous weld 55 is preferably applied about the entire length of the axle seat periphery, thereby reducing the number of weld ends and increasing the durability of the axle connection. Specifically, welding about the entire axle seat periphery between theaxle adapter 36 and theaxle 48, reduces stress risers associated with using multiple welds, and allows a relatively thin axle wall to be utilized. As best illustrated inFIG. 8 , theforward weld ears 50 and rearwardweld ears 52 are positioned and configured with regards to the associatedaxle 14 such that theweld 55 positioned proximate a leadingedge 65 of theforward weld ears 50 preferably forms a negative angle a with the horizontal of between about 30° to about 45°, and more preferably of about 35°, and such that theweld 55 positioned proximate atrailing edge 67 of the rearwardweld ears 52 preferably forms a positive angle β the horizontal of between about 25° and about 45°, and more preferably of about 8°, thereby reducing the stress exerted on the axle connection by typical operational loads. The location of theweld ears weld ears welds 55. - The air spring support 30 (
FIGS. 3-6 ) of thetrailing arm assembly 12 includes a top plate orspring support plate 56 upon which the associatedair spring assembly 28 is supported, and a pair ofsupport brackets 58 extending between thesecond end 21 of thetrailing arm 18 and thetop plate 56. Specifically, eachsupport bracket 58 is generally triangularly shaped and includes aforward edge 60 weldably secured to arearward face 61 of thesecond end 21 of thetrailing beam 18, atop edge 62 weldably secured to an underside of thetop plate 56, and a downwardly facingedge 64. Thetop plate 56 is positioned with respect to thesupport brackets 58 such that aforward edge portion 66 of thetop plate 56 overlies theupper flange 44 of thetrailing arm 18. Theforward edge portion 66 includes awelding window 68 which receives a weld, thereby securing thetop plate 56 to the trailingarm assembly 12. It is noted that theweld window 68 is located on an outboard side of thetop plate 56 such that thetop plate 56 is welded to a draft surface of thetrailing arm 18, thereby causing thetop plate 56 to “tilt” to the outboard side of thetrailing arm 18. Specifically, thespring supporting surface 57 of thetop plate 56 is outwardly canted with regards to at least one of the central axis member 39 and the central axis of thepivot axis 26 at an angle ∞ of preferably within the range of between about 0.5° and about 3°; and more preferably within the range of between about 0.5° and 1.5°. As a result, loading of theoverall suspension system 10 causes the overalltrailing arm assembly 12 to “tilt” inboard such that the top plate or airspring mounting plate 56 is substantially parallel to upper air spring mounting plates 70 (FIG. 1 ) attached to theframe member 24. The resulting parallel relationship between thetop plate 56 and the associated upper airspring mounting plate 70 reduces the wear exerted on theair spring assembly 28 during operation. - The
reference numeral 12 a (FIGS. 9-11 b) generally designates another embodiment of the trailing arm assembly of the present invention. Since thetrailing arm assembly 12 a is similar to the previously described embodiment of thetrailing arm assembly 12, similar parts appearing inFIGS. 1-8 andFIGS. 9-11 b respectively are represented by the same, corresponding reference numeral, except for the suffix “a” in the numerals of the latter. In the illustrated example, the trailingarm assembly 12 a includes the trailingarm 18 a and theair spring support 30 a. Thesecond end 21 a of the trailing arm includes a pair of rearwardly extending eyelets or hingemembers 100 having bolt-receivingapertures 102 extending therethrough. Theair spring support 20 a is generally arcuately-shaped and includes a forwardly-extendingcoupling portion 104 and a rearwardly-locatedspring support plate 56 a. Thecoupling portion 104 includes a pair of laterally-spacedplate portions 106 that flank thehinge members 100 and includeapertures 108 that correspond to theapertures 102 and that receivebolts 110, thereby coupling theair spring support 20 a with the trailingarm member 18 a. Theend surface 111 of the trailingarm 18 a is machined and abuts amachined surface 113 of theair spring support 30 a, so as to support downward forces exerted by theair spring 28 onto theair spring support 30 a. - The
reference numeral 12 b (FIGS. 12-14 ) generally designates another embodiment of the trailing arm assembly of the present invention. Since the trailingarm assembly 12 b is similar to the previously described embodiment of the trailingarm assembly 12, similar parts appearing inFIGS. 1-8 andFIGS. 12-14 respectively are represented by the same, corresponding reference numeral, except for the suffix “b” in the numerals of the latter. In the illustrated example, the trailingarm assembly 12 b includes the trailingarm 18 b and theair spring support 30 b. Thesecond end 21 b of the trailingarm 18 b is rearwardly, downwardly sloped and is defined by arearward surface 80 and aledge 82 that is vertically offset below an uppermost surface of the trailingarm 18 b. Theforward edge 60 b of each of thesupport brackets 58 b of theair spring support 30 b has a forwardly-opening concave shape that is positioned about a complimentary convex shape of therearward surface 80 of the trailingarm 18 b. Theforward edge portion 66 b of thetop plate 56 b cantilevers and extends over theledge 82 of thesecond end 21 b of the trailingarm 18 b and is secured thereto via a weld located within thewelding window 68 b. Theair spring support 30 b is further secured to the associated trailingarm 18 b viawelds 84, while thetop plate 56 b and thesupport brackets 58 b are secured to one another via a plurality ofwelds 86. This particular configuration allows the overall height of the trailingarm assembly 12 b to be minimized, and allows vertical loads from theair spring assemblies 28 to be supported by the trailingarm 18 b through compressive stresses within theledge 82 andrearward surface 80 of the trailingarm 18 b. - The
reference numeral 18 c (FIGS. 15-17 ) generally designates another embodiment of the trailing arm of the present invention. Since the trailingarm 18 c is similar to the previously described embodiment of the trailingarm 18, similar parts appearing inFIGS. 3-6 andFIGS. 15-17 respectively are represented by the same, corresponding reference numeral, except for the suffix “c” in the numerals of the latter. As best illustrated inFIGS. 16 and 17 , the overall height h defined between an uppermost portion of therecess 46 c and the substantially perpendicularly located upper surface of the trailingarm 18 c is reduced. This reduction in overall height is accomplished by providing a relativelythick portion 40 c′ to theweb portion 40 c of the trailingarm 18 c proximate therecess 46 c, whereat theportion 40 c of theweb portion 40 c has a relatively greater thickness t″ compared to the thickness t′ of theweb portion 40 c extending along the remaining length of the trailingbeam 18 c. Preferably, the thickness t″ is between 2 and 8 times greater than the thickness t′. It is noted that the trailingarm 18 c does not include vertically extending reinforcement webs proximate to the forward edge of therecess 46 c, thereby providing a reduction in the overall weight of the trailingarm 18 c. - The
reference numeral 18 d (FIG. 18 ) generally designates yet another embodiment of the trailing arm of the present invention. Since the trailingarm 18 d is similar to the previously described embodiment of the trailingarm 18, similar parts appearing inFIGS. 3-6 andFIG. 18 respectively are represented by the same, corresponding reference numeral, except for the suffix “d” in the numerals of the latter. The trailingarm 18 d is provided with an overall curvalinear body shape thereby allowing “nesting” of a plurality of trailingarms 18 d with one another within an associatedcasting core box 88. The nesting of the trailingarms 18 d with one another reduces the overall area required within thecasting core box 88, thereby increasing yield per mold during the casting process, resulting in a reduction in costs for manufacturing each beam and increasing the overall efficiency of the foundry. - The present inventive trailing arm assembly and related suspension system increases the durability of the associated axle connection, while simultaneously reducing the weight. The trailing arm assembly and suspension system is efficient in assembly and use, is capable of a long operating life, and is particularly well adapted for the proposed use.
- The above description is considered that of the preferred embodiments only. Modifications of the invention will occur to those skilled in the art and to those who make or use the invention. Therefore, it is understood that the embodiments shown in the drawings and described above are merely for illustrative purposes and not intended to limit the scope of the invention, which is defined by the following claims as interpreted according to the principles of patent law, including the doctrine of equivalents.
Claims (13)
Priority Applications (2)
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US14/294,853 US9352627B2 (en) | 2011-03-28 | 2014-06-03 | Trailing arm suspension beam assembly |
US15/083,981 US10029527B2 (en) | 2011-03-28 | 2016-03-29 | Trailing arm suspension assembly |
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US201161468359P | 2011-03-28 | 2011-03-28 | |
US14/007,874 US8910961B2 (en) | 2011-03-28 | 2012-03-27 | Trailing arm suspension beam assembly |
PCT/US2012/030715 WO2012135200A2 (en) | 2011-03-28 | 2012-03-27 | Trailing arm suspension beam assembly |
US14/294,853 US9352627B2 (en) | 2011-03-28 | 2014-06-03 | Trailing arm suspension beam assembly |
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US14/007,874 Continuation US8910961B2 (en) | 2011-03-28 | 2012-03-27 | Trailing arm suspension beam assembly |
PCT/US2012/030715 Continuation WO2012135200A2 (en) | 2011-03-28 | 2012-03-27 | Trailing arm suspension beam assembly |
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US15/083,981 Continuation US10029527B2 (en) | 2011-03-28 | 2016-03-29 | Trailing arm suspension assembly |
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US14/294,853 Active 2032-05-16 US9352627B2 (en) | 2011-03-28 | 2014-06-03 | Trailing arm suspension beam assembly |
US15/083,981 Active 2032-06-15 US10029527B2 (en) | 2011-03-28 | 2016-03-29 | Trailing arm suspension assembly |
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US (3) | US8910961B2 (en) |
EP (2) | EP2691249B1 (en) |
CN (1) | CN103476609B (en) |
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BR (1) | BR112013023906A2 (en) |
CA (1) | CA2827780C (en) |
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MX348688B (en) | 2011-03-28 | 2017-06-26 | Saf-Holland Inc | Trailing arm suspension beam assembly. |
DE102013210142A1 (en) | 2013-05-31 | 2014-12-04 | Saf-Holland Gmbh | handlebar unit |
DE102013214737A1 (en) * | 2013-07-29 | 2015-01-29 | Saf-Holland Gmbh | handlebar unit |
DE102013218028B4 (en) * | 2013-09-10 | 2015-12-03 | Saf-Holland Gmbh | axle connection |
DE102014218323B4 (en) | 2014-09-12 | 2020-12-31 | Saf-Holland Gmbh | Axle unit |
DE102014218317B4 (en) * | 2014-09-12 | 2020-03-26 | Saf-Holland Gmbh | Axle unit |
DE102014218315A1 (en) * | 2014-09-12 | 2016-03-17 | Saf-Holland Gmbh | link element |
DE102014218325B4 (en) * | 2014-09-12 | 2021-10-28 | Saf-Holland Gmbh | Axle unit |
CN104442253B (en) * | 2014-11-18 | 2017-07-21 | 重庆永淳新能源科技有限公司 | Rear-guard formula rear axle of electric automobile power transmission structure |
DE102015209001B4 (en) * | 2015-05-15 | 2017-02-23 | Ford Global Technologies, Llc | Wheel suspension unit for a motor vehicle |
USD770346S1 (en) * | 2015-06-16 | 2016-11-01 | Haldex Brake Products Ab | Brake adjuster |
USD770344S1 (en) * | 2015-06-16 | 2016-11-01 | Haldex Brake Products Ab | Brake adjuster |
USD770343S1 (en) * | 2015-06-16 | 2016-11-01 | Haldex Brake Products Ab | Brake adjuster |
USD770345S1 (en) * | 2015-06-16 | 2016-11-01 | Haldex Brake Products Ab | Brake adjuster |
USD828250S1 (en) * | 2015-08-31 | 2018-09-11 | Cummins Inc. | Compression relief brake system |
USD813124S1 (en) * | 2015-08-31 | 2018-03-20 | Cummins Inc. | Rocker for compression relief brake |
USD808872S1 (en) * | 2015-09-11 | 2018-01-30 | Eaton S.R.L. | Rocker arm for engine brake |
USD801895S1 (en) * | 2015-09-22 | 2017-11-07 | Saf-Holland, Inc. | Brake torque plate |
EP3429872A4 (en) * | 2016-03-17 | 2019-11-13 | SAF-Holland, Inc. | Powered vehicle suspension assembly |
DE102016111990B4 (en) | 2016-06-30 | 2022-05-05 | Saf-Holland Gmbh | handlebar system |
CN106627014B (en) * | 2016-11-22 | 2018-12-28 | 广州市特耐得车轴有限公司 | A kind of axle trailing arm and its welding method |
WO2021056079A1 (en) * | 2019-09-27 | 2021-04-01 | Cruisemaster Australia Pty Ltd | Improvement to independent suspension with airbag |
USD956536S1 (en) * | 2020-05-08 | 2022-07-05 | Array Technologies, Inc. | Mounting hardware |
USD956537S1 (en) | 2020-05-08 | 2022-07-05 | Array Technologies, Inc. | Mounting hardware |
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2012
- 2012-03-27 MX MX2013011029A patent/MX348688B/en active IP Right Grant
- 2012-03-27 CA CA2827780A patent/CA2827780C/en active Active
- 2012-03-27 US US14/007,874 patent/US8910961B2/en active Active
- 2012-03-27 BR BR112013023906A patent/BR112013023906A2/en not_active IP Right Cessation
- 2012-03-27 CN CN201280015638.1A patent/CN103476609B/en active Active
- 2012-03-27 WO PCT/US2012/030715 patent/WO2012135200A2/en active Application Filing
- 2012-03-27 AU AU2012236747A patent/AU2012236747B2/en not_active Ceased
- 2012-03-27 EP EP12763414.5A patent/EP2691249B1/en active Active
- 2012-03-27 EP EP15167475.1A patent/EP2946952B1/en active Active
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2013
- 2013-09-25 MX MX2015016414A patent/MX345592B/en unknown
-
2014
- 2014-06-03 US US14/294,853 patent/US9352627B2/en active Active
-
2016
- 2016-03-29 US US15/083,981 patent/US10029527B2/en active Active
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US20010020775A1 (en) * | 1998-07-02 | 2001-09-13 | Pierce Phillippi R. | Trailing arm axle/suspension system |
US20040051268A1 (en) * | 2000-09-05 | 2004-03-18 | David Chan | Connection between vehicle axle and suspension arm |
US7048288B2 (en) * | 2000-09-05 | 2006-05-23 | Meritor Heavy Vehicle Systems Limited | Vehicle suspension beam |
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Also Published As
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US9352627B2 (en) | 2016-05-31 |
CN103476609A (en) | 2013-12-25 |
CA2827780C (en) | 2019-03-12 |
MX348688B (en) | 2017-06-26 |
AU2012236747B2 (en) | 2016-05-12 |
EP2691249A4 (en) | 2014-08-27 |
US8910961B2 (en) | 2014-12-16 |
CA2827780A1 (en) | 2012-10-04 |
US10029527B2 (en) | 2018-07-24 |
AU2012236747A1 (en) | 2013-09-12 |
MX2013011029A (en) | 2013-11-20 |
WO2012135200A2 (en) | 2012-10-04 |
BR112013023906A2 (en) | 2019-09-24 |
EP2691249A2 (en) | 2014-02-05 |
EP2946952B1 (en) | 2019-10-02 |
WO2012135200A3 (en) | 2012-12-27 |
EP2691249B1 (en) | 2017-08-23 |
EP2946952A1 (en) | 2015-11-25 |
US20140015214A1 (en) | 2014-01-16 |
CN103476609B (en) | 2015-12-02 |
MX345592B (en) | 2017-02-07 |
US20160250904A1 (en) | 2016-09-01 |
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